Patents by Inventor Mathieu Lannuzel

Mathieu Lannuzel has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 10105938
    Abstract: The disclosure proposes a method for producing a panel having an outer skin and stiffeners that have a connecting portion, and at least one projecting portion, the method comprising a step of draping layers of fibers over at least one insert such that each layer of fibers has a connecting portion and a portion that projects downwardly from the connecting portion, a step of draping a layer of fibers that forms the outer skin, and a step of bonding the layers of fibers together. The disclosure also provides a device for implementing the method.
    Type: Grant
    Filed: December 1, 2014
    Date of Patent: October 23, 2018
    Assignee: Airbus Operations (S.A.S.)
    Inventors: Dominique Guittard, Mathieu Lannuzel, Philippe Blot, Gilles Bezard
  • Patent number: 9073272
    Abstract: A process for the production of a fiber profile (32) that is designed to fill in a space with a nail-head-shaped or half-nail-head-shaped cross-section that originates from the assembly of preforms in a T shape, of which at least one includes a curvature radius at the junction zone of the preforms, includes: supplying powder-coated fibers (28) to a preforming station (30) where the powder is activated and the fibers (28) move into a passage whose shapes are adapted to those of the desired profile, and then making the preformed fibers move into a shaping station (34) where the fiber profile (32) is cooled and shaped by circulating in a cavity whose shapes are adapted to those of the desired profile.
    Type: Grant
    Filed: June 25, 2010
    Date of Patent: July 7, 2015
    Assignee: AIRBUS OPERATIONS, SAS
    Inventors: Philippe Blot, Mathieu Lannuzel, Pascal Vinot
  • Publication number: 20150165744
    Abstract: The disclosure proposes a method for producing a panel having an outer skin and stiffeners that have a connecting portion, and at least one projecting portion, the method comprising a step of draping layers of fibers over at least one insert such that each layer of fibers has a connecting portion and a portion that projects downwardly from the connecting portion, a step of draping a layer of fibers that forms the outer skin, and a step of bonding the layers of fibers together. The disclosure also provides a device for implementing the method.
    Type: Application
    Filed: December 1, 2014
    Publication date: June 18, 2015
    Inventors: Dominique Guittard, Mathieu Lannuzel, Philippe Blot, Gilles Bezard
  • Patent number: 8852495
    Abstract: A process for manufacturing a piece made of composite material including a fiber preform that is embedded in a matrix, includes placing the preform in a first chamber that is delimited by a first semi-sealed wall, i.e., permeable to gas and impermeable to a product that is able to form the matrix, extracting the gases in a second chamber that is delimited by a second gas-tight wall and the first semi-sealed wall so as to obtain the diffusion of the product that is able to form the matrix in the preform, characterized in that it consists in using—as a first semi-sealed wall—at least one plate with a number of pipes of tapered shape that empty on either side of the at least one plate and at least one semi-sealed membrane that is superposed on the at least one plate.
    Type: Grant
    Filed: August 6, 2009
    Date of Patent: October 7, 2014
    Assignee: Airbus Operations SAS
    Inventors: Philippe Blot, Sébastien Gohier, Mathieu Lannuzel
  • Patent number: 8628709
    Abstract: A process for manufacturing a piece made of composite material with a hollow form and including a fiber preform (50) that is embedded in a matrix, includes placing the preform (50) in a first chamber (64) delimited by a mold (52) that is in contact with the surface of the piece to be produced outside of the hollow form and a counter-mold (54) that is in contact with the surface of the piece to be produced inside of the hollow form, and using a mold (52) that is made in at least two parts (52.1, 52.2) and elements (78) for controlling the spacing of the at least two parts (52.1, 52.2) that are contiguous using the expansion phenomenon during the polymerization phase.
    Type: Grant
    Filed: October 2, 2009
    Date of Patent: January 14, 2014
    Assignee: Airbus Operations SAS
    Inventors: Philippe Blot, Sebastien Gohier, Mathieu Lannuzel
  • Patent number: 8562780
    Abstract: A process for the production of a stiffened panel made of composite material includes the stages of depositing the fibers that constitute the panel on a rigid device, depositing at least one stiffener, covering the unit with a sealed wall, and then polymerizing, and providing—for each stiffener—a rigid counter-mold in contact with the convex surface of the stiffener, covering the zone(s) of the panel that is/are not covered by the stiffener with at least one band sufficiently rigid to transmit compression forces by allowing play between the band and the stiffener, and then depositing a seal such that the seal, the band, and the rigid counter-mold form the sealed wall, whereby the seal is able to have two states, a first malleable state during application so that it adapts to the profile of the lateral edges of the stiffeners, and a hardened state to ensure transmission of compression forces in a manner essentially identical to the rigid counter-molds or to the bands arranged on either side of the seal so as n
    Type: Grant
    Filed: July 20, 2011
    Date of Patent: October 22, 2013
    Assignee: Airbus Operations SAS
    Inventors: Denis De Mattia, Mathieu Lannuzel
  • Publication number: 20120237736
    Abstract: A process for the production of a fiber profile (32) that is designed to fill in a space with a nail-head-shaped or half-nail-head-shaped cross-section that originates from the assembly of preforms in a T shape, of which at least one includes a curvature radius at the junction zone of the preforms, includes: supplying powder-coated fibers (28) to a preforming station (30) where the powder is activated and the fibers (28) move into a passage whose shapes are adapted to those of the desired profile, and then making the preformed fibers move into a shaping station (34) where the fiber profile (32) is cooled and shaped by circulating in a cavity whose shapes are adapted to those of the desired profile.
    Type: Application
    Filed: June 25, 2010
    Publication date: September 20, 2012
    Applicant: AIRBUS OPERATIONS SAS
    Inventors: Philippe Blot, Mathieu Lannuzel, Pascal Vinot
  • Publication number: 20120024455
    Abstract: A process for the production of a stiffened panel made of composite material includes the stages of depositing the fibers that constitute the panel on a rigid device, depositing at least one stiffener, covering the unit with a sealed wall, and then polymerizing, and providing—for each stiffener—a rigid counter-mold in contact with the convex surface of the stiffener, covering the zone(s) of the panel that is/are not covered by the stiffener with at least one band sufficiently rigid to transmit compression forces by allowing play between the band and the stiffener, and then depositing a seal such that the seal, the band, and the rigid counter-mold form the sealed wall, whereby the seal is able to have two states, a first malleable state during application so that it adapts to the profile of the lateral edges of the stiffeners, and a hardened state to ensure transmission of compression forces in a manner essentially identical to the rigid counter-molds or to the bands arranged on either side of the seal so as n
    Type: Application
    Filed: July 20, 2011
    Publication date: February 2, 2012
    Applicant: AIRBUS OPERATIONS (SAS)
    Inventors: Denis DE MATTIA, Mathieu LANNUZEL
  • Publication number: 20110272852
    Abstract: A process for manufacturing a piece made of composite material with a hollow form and including a fiber preform (50) that is embedded in a matrix, includes placing the preform (50) in a first chamber (64) delimited by a mold (52) that is in contact with the surface of the piece to be produced outside of the hollow form and a counter-mold (54) that is in contact with the surface of the piece to be produced inside of the hollow form, and using a mold (52) that is made in at least two parts (52.1, 52.2) and elements (78) for controlling the spacing of the at least two parts (52.1, 52.2) that are contiguous using the expansion phenomenon during the polymerization phase.
    Type: Application
    Filed: October 2, 2009
    Publication date: November 10, 2011
    Applicant: AIRBUS OPERATIONS SAS
    Inventors: Philippe Blot, Sebastien Gohier, Mathieu Lannuzel
  • Publication number: 20110180960
    Abstract: A process for manufacturing a piece made of composite material including a fiber preform that is embedded in a matrix, includes placing the preform in a first chamber that is delimited by a first semi-sealed wall, i.e., permeable to gas and impermeable to a product that is able to form the matrix, extracting the gases in a second chamber that is delimited by a second gas-tight wall and the first semi-sealed wall so as to obtain the diffusion of the product that is able to form the matrix in the preform, characterized in that it consists in using—as a first semi-sealed wall—at least one plate with a number of pipes of tapered shape that empty on either side of the at least one plate and at least one semi-sealed membrane that is superposed on the at least one plate.
    Type: Application
    Filed: August 6, 2009
    Publication date: July 28, 2011
    Applicant: AIRBUS OPERATIONS
    Inventors: Philippe Blot, Sebastien Gohier, Mathieu Lannuzel